Engineering:Meadowcroft Chinook
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Revision as of 10:24, 8 April 2022 by imported>Carolyn (add)
| Meadowcroft Chinook | |
|---|---|
| Role | Homebuilt aircraft |
| National origin | United States of America |
| Designer | Bill Meadowcroft |
| First flight | 1958 |
| Number built | 1 |
The Meadowcroft Chinook is a two-seat mid-winged American homebuilt aircraft design first flown in 1958.[1]
Development
The Chinook was designed for maximum stability on the ground and the air with a roomy cockpit.
Design
The wing was patterned from the Ace Baby Ace homebuilt. The aircraft is a tricycle geared side-by-side seat mid-winged aircraft with a steeply raked windscreen. Each wing is braced with two small wing struts attached to the lower fuselage. The low rudder is capped with a strut braced horizontal stabilizer in a T-tail arrangement. The main gear is sourced from a Cessna 140. The aircraft can be reconfigured to be towed on its main gear by a vehicle.[2]
Specifications (Meadowcroft Chinook)
Data from Sport Aviation
General characteristics
- Capacity: 2
- Airfoil: NACA 23012
- Powerplant: 1 × Continental C-90-12F , 90 hp (67 kW)
- Propellers: <2!-- propeller aircraft -->-bladed McCaulley
Performance
- Cruise speed: 109 kn (125 mph, 201 km/h)
References
- ↑ "N2879D". http://www.airport-data.com/aircraft/N2879D.html. Retrieved 18 October 2011.
- ↑ Sport Aviation. November 1960.
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